Venkat Narayanaswamy
Professor
- Phone: (919) 515-7544
- Email: vnaraya3@ncsu.edu
- Office: Engineering Building III (EB3) 3298
- Website: http://www4.ncsu.edu/~vnaraya3/
Dr. Venkat Narayanaswamy is interested in scramjet propulsion, laser diagnostics, and combustion. Prior to joining NC State, he was a Postdoctoral Research Associate at UT Austin and RWTH Aachen, Germany. Dr. Narayanaswamy’s long term vision is contributing to the development of next-generation clean and efficient propulsion technologies.
Outside research, Dr. Narayanaswamy is interested in nature photography.
Publications
- Dual separation control and drag mitigation in high speed flows using viscoelastic materials
- Walz, J., & Narayanaswamy, V. (2023), Physics of Fluids, 35(3), 031704. https://doi.org/10.1063/5.0141572
- Fluid structure interactions generated by an oblique shock impinging on a thin elastic panel
- Varigonda, S. V., & Narayanaswamy, V. (2023), JOURNAL OF FLUIDS AND STRUCTURES, 119. https://doi.org/10.1016/j.jfluidstructs.2023.103890
- Investigations of shock-boundary layer interaction dynamics using high-bandwidth pressure field imaging
- Jenquin, C., Johnson, E. C., & Narayanaswamy, V. (2023), JOURNAL OF FLUID MECHANICS, 961. https://doi.org/10.1017/jfm.2023.168
- Quenching measurements of Kr 5p[3/2](2) <- <- 4p(61)S(0) electronic transition using absorption spectra
- Sahoo, A., Narayanaswamy, V., & Lyons, K. M. (2023), APPLIED OPTICS, 62(6), 110–117. https://doi.org/10.1364/AO.475382
- Effects of Pressure Sensitive Paint on the Dynamics of Half-Inlet Shock Dynamics
- Jenquin, C., Johnson, E., & Narayanaswamy, V. (2022), AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022, 1–13. https://doi.org/10.2514/6.2022-0068
- Experimental Investigations of the Hypersonic Stream-Traced Performance Inlet at Subdesign Mach Number
- Johnson, E., Jenquin, C., McCready, J., Narayanaswamy, V., & Edwards, J. (2022, September 30), AIAA JOURNAL, Vol. 61. https://doi.org/10.2514/1.J062113
- Experimental Studies of Unstart Shock Dynamics within a Streamtraced Scramjet Inlet
- Johnson, E., Jenquin, C., & Narayanaswamy, V. (2022), AIAA AVIATION 2022 Forum. https://doi.org/10.2514/6.2022-3478
- Fluid Structure Interactions Generated by an Oblique Shock Impinging on a Thin Elastic Panel
- Narayanaswamy, V., & Varigonda, S. V. (2022), SSRN. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-85145488659&partnerID=MN8TOARS
- Investigations of Shock Boundary Layer Interactions Over a Soft Material for Separated Control
- Walz, J., & Narayanaswamy, V. (2022), AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022. https://doi.org/10.2514/6.2022-0605
- Investigations of the Transition Between Conventional and Distributed Regime in Turbulent Jet Flames
- Deboskey, R., Kessler, D., Johnson, R. F., Bojko, B., Sahoo, A., Narayanaswamy, V., & Lyons, K. M. (2022), AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022. https://doi.org/10.2514/6.2022-2089
Grants
- High Speed Morphing Propulsion Concepts to Advance Range, Efficiency and Maneuverability (ARL-BAA no. W911NF-17-S-0003-11, section: e. CCE-ScMVR-2(iv))
- Test Rig for Effective Reproduction of Inlet Distorted Supersonic Flows
- Variable Engine for New Maneuvers
- Long duration Mach 6 wind tunnel facility for hypersonics research
- Demonstration of a Gas Turbine Scale RDC Integrated with Compressor and Turbine Conditions at 7FA Cycle.
- Investigations of Self Starting Streamtraced Inlets at Off-Design Conditions
- Fluid Structure Interactions between unsteady shock waves and compliant materials for unsteady load mitigation
- Tailored Supersonic Flowfields
- Fluid Structural Thermal Interactions (FSTI) in Hypersonic Flow
- Non-intrusive Flight Trajectory Manipulation of High-speed Munitions Using Non-linear Shock/Boundary Layer Interactions
